US8308526B2 - Masking method for edge profile finishing - Google Patents

Masking method for edge profile finishing Download PDF

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Publication number
US8308526B2
US8308526B2 US13/338,322 US201113338322A US8308526B2 US 8308526 B2 US8308526 B2 US 8308526B2 US 201113338322 A US201113338322 A US 201113338322A US 8308526 B2 US8308526 B2 US 8308526B2
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United States
Prior art keywords
mask
media
edge
airfoil
finishing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
US13/338,322
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US20120094580A1 (en
Inventor
Navabalachandran Jayabalan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pratt and Whitney Services Pte Ltd
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Pratt and Whitney Services Pte Ltd
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Publication date
Application filed by Pratt and Whitney Services Pte Ltd filed Critical Pratt and Whitney Services Pte Ltd
Priority to US13/338,322 priority Critical patent/US8308526B2/en
Publication of US20120094580A1 publication Critical patent/US20120094580A1/en
Application granted granted Critical
Publication of US8308526B2 publication Critical patent/US8308526B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B19/00Single-purpose machines or devices for particular grinding operations not covered by any other main group
    • B24B19/14Single-purpose machines or devices for particular grinding operations not covered by any other main group for grinding turbine blades, propeller blades or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B31/00Machines or devices designed for polishing or abrading surfaces on work by means of tumbling apparatus or other apparatus in which the work and/or the abrasive material is loose; Accessories therefor
    • B24B31/12Accessories; Protective equipment or safety devices; Installations for exhaustion of dust or for sound absorption specially adapted for machines covered by group B24B31/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making

Definitions

  • This application relates to a mask for a trailing edge of an airfoil.
  • Airfoils such as used as compressor blades for gas turbine engines, are in part formed with a shearing operation.
  • the leading edge of the airfoil is initially an unprofiled blunt edge after the shearing operation.
  • the airfoil and the rest of the blade are placed in a high speed media finishing centrifuge.
  • Media is directed at high speed toward the leading edge such that the initial blunt edge is formed into a smoother rounded edge in a final desired shape that helps facilitate airflow.
  • small stones are moved at a high speed toward the leading edge to create the rounded surface.
  • the tape does protect the airfoil, the tape does not serve to direct the media toward the leading edge. Instead, the thin vinyl tape only serves to protect the non-repaired area from erosion by preventing contact from media.
  • a mask for a trailing edge of an airfoil is formed to have a slot extending from an open end inwardly to an inner end.
  • a thicker portion of the mask is spaced further away from the open end and thinner portions are spaced toward the open end. The thicker portion of the mask serves to redirect media stones toward the leading edge, thus creating a more efficient media finishing operation.
  • FIG. 1 is a perspective view of a blade and mask.
  • FIG. 2 is a schematic view of the mask and blade within a centrifuge.
  • FIG. 3 shows the removal of the mask from the blade.
  • FIG. 1 An exemplary blade and mask system 20 is illustrated in FIG. 1 .
  • the blade 22 has a platform and root section 24 , and an airfoil 26 .
  • the airfoil 26 has a leading edge 28 and a trailing edge 27 .
  • the airfoil 26 is formed from an initial metal medium using a shearing operation such that a blunt shearing edge 30 remains after the shearing operation.
  • a media finishing operation is performed to round the shearing edge of the intermediate part to the final leading edge 28 .
  • a mask 32 is mounted on the trailing edge 27 during this tumbling operation.
  • the blade 22 is slipped into the pre-fabricated masking “fixture” by being moved into slot 38 .
  • a centrifuge tumbling system 50 is used for a media finishing the airfoil 26 .
  • the mask 32 has thicker portions 36 more removed from the leading edge 28 than thinner portions 34 , which are spaced toward the leading edge 28 .
  • an outer periphery surface of the mask 32 is substantially curved at the thicker portions 36 and tapers inwardly towards the thinner portions 34 .
  • the media is now directed more toward the leading edge 28 and the shearing edge 30 to be removed.
  • one media stone 99 has struck the outer periphery surface of the mask 32 adjacent to thicker portion 36 . A trajectory of the stone 99 will now be changed toward the leading edge 28 .
  • the slot 38 has an open end 39 extending inwardly to an inner end 41 .
  • the trailing edge 27 of the airfoil extends into the inner end 41 .
  • the thinner portions 34 can be seen to be spaced toward the open end 39 relative to the thicker portions 36 .
  • the outer profile of the mask 32 from the thicker portions 36 leading to the thinner portions 34 is curved to guide the media 99 toward the blunt edge 30 to facilitate formation of the leading edge 28 . Shapes other than curves may be utilized.
  • the terms “thicker” and “thinner” are defined by the distance from the trailing edge 27 to an outer profile of the mask at the locations when the mask is received on an airfoil. While the thicker portion 36 may not redirect all of the media toward the blunt edge 30 , it will serve to redirect a good deal of the media towards the edge 30 .
  • the prior art tape which was of a thin, uniform width, would not direct any more media toward the edge than what may have been directed in some other direction.
  • the mask can be utilized with other tumbling machines for media and stock removal and for rounding operations.
  • vibratory tumbling machines could benefit from the disclosed mask.
  • the media finishing utilizing such a mask is done much more efficiently, in that the media is concentrated on the area to be finished.
  • the mask 32 can be easily removed from the airfoil 22 .
  • the mask 32 is preferably formed of a suitable material, such as rubber or plastic.
  • the mask can be made of a material that is flexible enough to mount the blade, but rigid enough not to deform under the media impact.
  • a rubber material that temporarily deforms to allow mounting and returns to original shape, and maintains its shape during the process was used.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Physical Vapour Deposition (AREA)
  • Centrifugal Separators (AREA)

Abstract

A mask for performing high speed media finishing on airfoils includes a thicker portion and a thinner portion. The thicker portion is spaced further from an edge that will become a leading edge in the final airfoil than the thinner portion. The media is redirected by the thicker portion toward the edge where the finishing is to occur.

Description

RELATED APPLICATIONS
This application is a divisional of U.S. application Ser. No. 12/045,093, filed Mar. 10, 2008, which claims priority to Singapore Application No. 200800203.2, filed Jan. 9, 2008.
BACKGROUND OF THE INVENTION
This application relates to a mask for a trailing edge of an airfoil.
Airfoils, such as used as compressor blades for gas turbine engines, are in part formed with a shearing operation. The leading edge of the airfoil is initially an unprofiled blunt edge after the shearing operation.
Typically, the airfoil and the rest of the blade are placed in a high speed media finishing centrifuge. Media is directed at high speed toward the leading edge such that the initial blunt edge is formed into a smoother rounded edge in a final desired shape that helps facilitate airflow. Essentially, small stones are moved at a high speed toward the leading edge to create the rounded surface.
In the prior art, the remainder of the airfoil which does not need rounding is masked by tape. Although the tape does protect the airfoil, the tape does not serve to direct the media toward the leading edge. Instead, the thin vinyl tape only serves to protect the non-repaired area from erosion by preventing contact from media.
SUMMARY OF THE INVENTION
In the disclosed embodiment of this invention, a mask for a trailing edge of an airfoil is formed to have a slot extending from an open end inwardly to an inner end. A thicker portion of the mask is spaced further away from the open end and thinner portions are spaced toward the open end. The thicker portion of the mask serves to redirect media stones toward the leading edge, thus creating a more efficient media finishing operation.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of a blade and mask.
FIG. 2 is a schematic view of the mask and blade within a centrifuge.
FIG. 3 shows the removal of the mask from the blade.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
An exemplary blade and mask system 20 is illustrated in FIG. 1. The blade 22 has a platform and root section 24, and an airfoil 26. In a final form, the airfoil 26 has a leading edge 28 and a trailing edge 27. Initially, the airfoil 26 is formed from an initial metal medium using a shearing operation such that a blunt shearing edge 30 remains after the shearing operation. Subsequently, a media finishing operation is performed to round the shearing edge of the intermediate part to the final leading edge 28. A mask 32 is mounted on the trailing edge 27 during this tumbling operation. As shown in the figure, the blade 22 is slipped into the pre-fabricated masking “fixture” by being moved into slot 38.
As shown in FIG. 2, a centrifuge tumbling system 50 is used for a media finishing the airfoil 26. The mask 32 has thicker portions 36 more removed from the leading edge 28 than thinner portions 34, which are spaced toward the leading edge 28. As shown, an outer periphery surface of the mask 32 is substantially curved at the thicker portions 36 and tapers inwardly towards the thinner portions 34. The media is now directed more toward the leading edge 28 and the shearing edge 30 to be removed. As shown schematically, one media stone 99 has struck the outer periphery surface of the mask 32 adjacent to thicker portion 36. A trajectory of the stone 99 will now be changed toward the leading edge 28.
As can be appreciated from FIGS. 2 and 3, the slot 38 has an open end 39 extending inwardly to an inner end 41. The trailing edge 27 of the airfoil extends into the inner end 41. The thinner portions 34 can be seen to be spaced toward the open end 39 relative to the thicker portions 36. As shown in the figures, the outer profile of the mask 32 from the thicker portions 36 leading to the thinner portions 34 is curved to guide the media 99 toward the blunt edge 30 to facilitate formation of the leading edge 28. Shapes other than curves may be utilized. Further, the terms “thicker” and “thinner” are defined by the distance from the trailing edge 27 to an outer profile of the mask at the locations when the mask is received on an airfoil. While the thicker portion 36 may not redirect all of the media toward the blunt edge 30, it will serve to redirect a good deal of the media towards the edge 30.
The prior art tape, which was of a thin, uniform width, would not direct any more media toward the edge than what may have been directed in some other direction.
While a centrifuge tumbling system is disclosed, the mask can be utilized with other tumbling machines for media and stock removal and for rounding operations. As an example, vibratory tumbling machines could benefit from the disclosed mask.
As compared to typical media finishing operations, the media finishing utilizing such a mask is done much more efficiently, in that the media is concentrated on the area to be finished.
As shown in FIG. 3, once the media finishing operation is complete, the mask 32 can be easily removed from the airfoil 22. The mask 32 is preferably formed of a suitable material, such as rubber or plastic. Generally, the mask can be made of a material that is flexible enough to mount the blade, but rigid enough not to deform under the media impact. In one embodiment, a rubber material that temporarily deforms to allow mounting and returns to original shape, and maintains its shape during the process was used.
Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.

Claims (2)

1. A method of finishing a blade having an airfoil, the method comprising the steps of:
a) providing an intermediate blade having an edge to be finished into a leading edge of the airfoil;
b) providing a mask having a slot extending from an open end to an inner end, and said mask having a thinner portion spaced toward said open end from a thicker portion, and positioning a trailing edge of said airfoil into said slot; and
c) placing said mask and said airfoil into a media finishing device, and directing media at the airfoil and mask, with said thicker portion of said mask directing media toward the edge of the intermediate blade.
2. The method as set forth in claim 1, wherein said media system is a centrifuge.
US13/338,322 2008-01-09 2011-12-28 Masking method for edge profile finishing Expired - Fee Related US8308526B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US13/338,322 US8308526B2 (en) 2008-01-09 2011-12-28 Masking method for edge profile finishing

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
SG200800203-2A SG154344A1 (en) 2008-01-09 2008-01-09 Airfoil mask, airfoil and mask system, and masking method for edge profile finishing
SG200800203.2 2008-01-09
US12/045,093 US8105133B2 (en) 2008-01-09 2008-03-10 Airfoil mask, airfoil and mask system
US13/338,322 US8308526B2 (en) 2008-01-09 2011-12-28 Masking method for edge profile finishing

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US12/045,093 Division US8105133B2 (en) 2008-01-09 2008-03-10 Airfoil mask, airfoil and mask system

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US20120094580A1 US20120094580A1 (en) 2012-04-19
US8308526B2 true US8308526B2 (en) 2012-11-13

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US12/045,093 Active 2030-10-12 US8105133B2 (en) 2008-01-09 2008-03-10 Airfoil mask, airfoil and mask system
US13/338,322 Expired - Fee Related US8308526B2 (en) 2008-01-09 2011-12-28 Masking method for edge profile finishing

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Application Number Title Priority Date Filing Date
US12/045,093 Active 2030-10-12 US8105133B2 (en) 2008-01-09 2008-03-10 Airfoil mask, airfoil and mask system

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US (2) US8105133B2 (en)
SG (1) SG154344A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110047777A1 (en) * 2009-08-27 2011-03-03 Soucy Ronald R Abrasive finish mask and method of polishing a component
WO2015027310A1 (en) * 2013-08-28 2015-03-05 Mds Coating Technologies Corp. Airfoil masking tool and method of polishing an airfoil
US9862057B2 (en) 2012-12-12 2018-01-09 United Technologies Corporation Vacuum degassing laser-blocking material system and process
US10406650B2 (en) 2013-08-28 2019-09-10 Mds Coating Technologies Corp. Airfoil masking tool and method of polishing an airfoil

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US20120171045A1 (en) * 2011-01-03 2012-07-05 United Technologies Corporation Turbine component fixture and coating system
SG195417A1 (en) 2012-06-01 2013-12-30 Pratt & Whitney Services Pte Ltd Polishing assembly and method for polishing
US9057272B2 (en) * 2012-06-29 2015-06-16 United Technologies Corporation Protective polishing mask
US9193111B2 (en) * 2012-07-02 2015-11-24 United Technologies Corporation Super polish masking of integrally bladed rotor
US9249490B2 (en) 2012-12-06 2016-02-02 United Technologies Corporation Mask system for gas turbine engine component
CN103084985B (en) * 2013-02-05 2015-08-12 浙江工业大学 A kind of ultra-precision processing apparatus retraining abrasive Flow
US9566603B2 (en) 2013-02-27 2017-02-14 United Technologies Corporation Split coating mask system for gas turbine engine component
WO2015006332A1 (en) * 2013-07-10 2015-01-15 United Technologies Corporation Vibratory mass media fixture with tip protector
EP3038794B1 (en) * 2013-08-28 2020-01-01 MDS Coating Technologies Corp. Airfoil masking tool and method of polishing an airfoil
WO2015088834A1 (en) * 2013-12-13 2015-06-18 United Technologies Corporation Integral part wear indicator system for stator
EP3225356B1 (en) * 2016-04-01 2023-03-01 Rolls-Royce plc Methods of vibro-treating and vibro-treating apparatus
EP3318750B1 (en) * 2016-11-02 2019-09-11 Caren Meicnic Teoranta An airfoil and a turbine apparatus
CN107186550B (en) * 2017-06-22 2018-03-13 中国科学院长春光学精密机械与物理研究所 A kind of processing method of curved slit
US20190194799A1 (en) 2017-12-22 2019-06-27 United Technologies Corporation Line-of-sight coating fixture and apparatus
US10792781B2 (en) * 2018-04-13 2020-10-06 Bell Helicopter Textron Inc. Masking tool system and method
US11566298B2 (en) * 2019-05-08 2023-01-31 Raytheon Technologies Corporation Systems and methods for manufacturing components for gas turbine engines

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110047777A1 (en) * 2009-08-27 2011-03-03 Soucy Ronald R Abrasive finish mask and method of polishing a component
US9862057B2 (en) 2012-12-12 2018-01-09 United Technologies Corporation Vacuum degassing laser-blocking material system and process
WO2015027310A1 (en) * 2013-08-28 2015-03-05 Mds Coating Technologies Corp. Airfoil masking tool and method of polishing an airfoil
US10406650B2 (en) 2013-08-28 2019-09-10 Mds Coating Technologies Corp. Airfoil masking tool and method of polishing an airfoil

Also Published As

Publication number Publication date
US20090173418A1 (en) 2009-07-09
US8105133B2 (en) 2012-01-31
US20120094580A1 (en) 2012-04-19
SG154344A1 (en) 2009-08-28

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